| 发明名称 |
Coolable airfoil attachment section |
| 摘要 |
A rotor blade suitable for use in a gas turbine engine includes an attachment section which defines at least one internal cooling passage along a passage axis through the attachment section. |
| 申请公布号 |
US8113784(B2) |
申请公布日期 |
2012.02.14 |
| 申请号 |
US20090407818 |
申请日期 |
2009.03.20 |
| 申请人 |
GUPTA SHIV C.;HAMILTON SUNDSTRAND CORPORATION |
发明人 |
GUPTA SHIV C. |
| 分类号 |
F01D5/30 |
主分类号 |
F01D5/30 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
|
| 地址 |
|
